US8273204B2 - Method for joining cellular acoustic panels - Google Patents

Method for joining cellular acoustic panels Download PDF

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Publication number
US8273204B2
US8273204B2 US12/864,377 US86437708A US8273204B2 US 8273204 B2 US8273204 B2 US 8273204B2 US 86437708 A US86437708 A US 86437708A US 8273204 B2 US8273204 B2 US 8273204B2
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Prior art keywords
acoustic panel
junction edge
acoustic
cells
mandrel
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Expired - Fee Related, expires
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US12/864,377
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English (en)
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US20100294422A1 (en
Inventor
Jean-Bernard Vache
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Safran Nacelles SAS
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Aircelle SA
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Assigned to AIRCELLE reassignment AIRCELLE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: VACHE, JEAN-BERNARD
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24—Heat or noise insulation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0044—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping edges or extremities
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B31—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31D—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER, NOT PROVIDED FOR IN SUBCLASSES B31B OR B31C
    • B31D3/00—Making articles of cellular structure, e.g. insulating board
    • B31D3/02—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section
    • B31D3/0292—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section involving auxiliary operations, e.g. expanding, moistening, glue-applying, joining, controlling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0081—Shaping techniques involving a cutting or machining operation before shaping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
    • B29C65/5057—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/022—Mechanical pre-treatments, e.g. reshaping
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/022—Mechanical pre-treatments, e.g. reshaping
    • B29C66/0222—Mechanical pre-treatments, e.g. reshaping without removal of material, e.g. cleaning by air blowing or using brushes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/114—Single butt joints
    • B29C66/1142—Single butt to butt joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/22—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being in the form of recurring patterns
    • B29C66/223—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being in the form of recurring patterns being in the form of a triangle wave or of a sawtooth wave, e.g. zigzagged
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/725—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0001—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular acoustical properties
    • B29K2995/0002—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular acoustical properties insulating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1003—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by separating laminae between spaced secured areas [e.g., honeycomb expanding]

Definitions

  • the present invention concerns a method for joining a first acoustic panel having a cellular structure of the honeycomb type, with a second panel.
  • This method is more particularly intended for the assembly of acoustic panels equipping a jet engine nacelle.
  • the nacelles are provided with acoustic panels aiming to attenuate the noise due to the circulation of flows of air through the jet engine as well as the vibrations of the structures of the nacelle.
  • the acoustic panels are of the sandwich-type structure well known for absorbing that noise. These panels usually include one or several layers of structures with a cellular core (structure commonly called “honeycomb”). The layers can then be coated on their so-called outer face, i.e. the face radially farthest from the axis of the engine, with an air-impermeable skin, called “full”, and on their inner face, i.e. that radially closest to the axis of the engine, with an air-permeable perforated skin, called “acoustic”.
  • the cellular core structure is realized from joined cellular units having cells of generally hexagonal or elliptical shape.
  • the acoustic properties of the acoustic panel i.e. its noise absorption rate depending on the frequency and noise level of the noise, depend in particular on the junction of the cellular unit(s).
  • the joining of the lateral ends is commonly done using a foaming glue, such as AFM 410® glue, which has a significant capacity for expansion.
  • AFM 410® glue which has a significant capacity for expansion.
  • the adjacent edges of the cellular unit(s) are coated with glue which, during its expansion, obstructs the cells by creating oversizes. These oversizes have the drawback of decreasing the effective acoustic surface of the cellular structure and also causing brutal impedance ruptures that contribute to decreasing the acoustic performance of the acoustic panel during the operation of the jet engine.
  • the cellular panels are cut to the required dimensions.
  • This cutting operation created a junction edge where the cells can be crushed and destroyed, which further decreases the final acoustic performance.
  • junction edges obtained have remains of cellular walls protruding from the junction edge and which will disrupt the thickness of the assembly zone.
  • edge to edge several cellular units by opening the cells situated on the edges designed to be joined and to overlap the cells as well as openings one in the other.
  • the present invention concerns a method for joining a first acoustic panel having a cellular structure of the honeycomb type and a second panel, comprising the steps of:
  • the connecting means is a gluing means.
  • the gluing means is a film of adhesive applied on at least one of the two junction edges.
  • the second panel is an acoustic panel having a cellular structure.
  • the steps of introducing at least one mandrel and passage of a roller are also done on the second acoustic panel.
  • a mandrel is introduced into each of the cells situated near the junction edge.
  • FIG. 1 is a diagrammatic view of a device allowing the implementation of the method.
  • FIG. 2 is a diagrammatic illustration of an acoustic panel after implementation of the method.
  • FIG. 3 is an illustration of two acoustic panels once joined.
  • FIG. 1 shows a device 1 for implementing the method according to the invention to join an acoustic panel 2 having a cellular structure comprising cells 3 of hexagonal shape.
  • This device comprises an upper plate 4 supporting a plurality of mandrels 5 each having a general section in the form of cells 3 and arranged regularly spaced such that each mandrel 5 can be introduced into every other cell 3 of a junction edge 6 of the acoustic panel 2 .
  • the device 1 also comprises a lower plate 7 also supporting a plurality of mandrels 8 each having a general section in cell form 3 and disposed regularly spaced such that each mandrel 8 can be introduced into every other cell 3 of the junction edge 6 of the acoustic panel 2 .
  • the device also comprises lower 9 and upper 10 plates for maintaining the acoustic panel each having openings 11 capable of being passed through by the mandrels 5 , 8 .
  • the device 1 lastly comprises a roller 12 situated so as to be able to roll along the junction edge 6 of the acoustic panel 2 .
  • the mandrels 5 , 8 of the upper 4 and lower 7 plates are introduced through the maintenance plates 9 , 10 and inside corresponding cells 3 .
  • Each mandrel 5 of the upper plate 4 therefore penetrates a cell 3 next to a cell 3 inside which a mandrel 8 of the lower plate 7 is introduced.
  • the introduction of the mandrels 5 , 8 inside cells 3 makes it possible to reshape them after any deformation or crushing due to the cutting of the acoustic panel 2 .
  • junction edge 6 is itself shaped owing to the roller 12 , which is passed all along the junction edge 6 .
  • any remains 60 of the cellular walls due to the cutting are flattened and crushed against the junction edge 6 .
  • the mandrels 5 , 8 make it possible for the roller 12 not to crush the cells during this shaping operation.
  • FIG. 2 A cellular acoustic panel 2 shaped using the device of FIG. 1 is shown in FIG. 2 .
  • the method is repeated on a second acoustic panel 2 ′ along a junction edge 6 ′.
  • junction of the two acoustic panels 2 , 2 ′ thus configured is traditionally done by application of an adhesive film on the junction edge and interlocking.
  • Two acoustic panels 2 , 2 ′ thus assembled are shown in FIG. 3 .
  • an acoustic panel can be joined to a non-acoustic panel, and other adhesive means can be used.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Laminated Bodies (AREA)
  • Building Environments (AREA)
US12/864,377 2008-01-23 2008-09-22 Method for joining cellular acoustic panels Expired - Fee Related US8273204B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0800346A FR2926614B1 (fr) 2008-01-23 2008-01-23 Procede de jonction de panneaux acoustiques alveolaires
FR0800346 2008-01-23
PCT/FR2008/001317 WO2009092870A1 (fr) 2008-01-23 2008-09-22 Procede de jonction de panneaux acoustiques alveolaires

Publications (2)

Publication Number Publication Date
US20100294422A1 US20100294422A1 (en) 2010-11-25
US8273204B2 true US8273204B2 (en) 2012-09-25

Family

ID=39684217

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/864,377 Expired - Fee Related US8273204B2 (en) 2008-01-23 2008-09-22 Method for joining cellular acoustic panels

Country Status (9)

Country Link
US (1) US8273204B2 (es)
EP (1) EP2254747B1 (es)
CN (1) CN101903160B (es)
BR (1) BRPI0821983A2 (es)
CA (1) CA2707851A1 (es)
ES (1) ES2388205T3 (es)
FR (1) FR2926614B1 (es)
RU (1) RU2469852C2 (es)
WO (1) WO2009092870A1 (es)

Cited By (1)

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Publication number Priority date Publication date Assignee Title
US20110290333A1 (en) * 2009-02-05 2011-12-01 Aircelle Method for manufacturing a structure with cellular cores for a turbojet nacelle

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GB2458679B (en) * 2008-03-28 2010-04-21 Rolls Royce Plc Acoustic liners
EP2295216B1 (de) 2009-09-15 2016-01-06 INVENT Innovative Verbundwerkstoffe Realisation und Vermarktung neuer Technologien GmbH Verfahren zur Herstellung einer Wabenstruktur aus einem Faserhalbzeug
EP2531665B1 (en) * 2010-02-05 2015-08-26 Bell Helicopter Textron Inc. Apparatus for attaching a member to a honeycomb core-stiffened structure
FR2975943B1 (fr) * 2011-06-01 2013-05-17 Aircelle Sa Procede de fabrication d'un panneau d'attenuation acoustique
US9365022B2 (en) * 2013-06-11 2016-06-14 Bell Helicopter Textron Inc. System and method of post-cure processing of composite core
US9068345B2 (en) * 2013-08-12 2015-06-30 Hexcel Corporation Multi-sectional acoustic septum
FR3041998B1 (fr) * 2015-10-01 2018-09-07 Aircelle Sa Panneau d’attenuation acoustique a structure a ame alveolaire imbriquee
US9779715B1 (en) * 2016-07-26 2017-10-03 Hexcel Corporation Method for making contoured acoustic structures
CN107639884B (zh) * 2017-08-09 2019-05-21 中国航空工业集团公司基础技术研究院 一种无缝拼接蜂窝芯材的制备方法
US20210256947A1 (en) * 2020-02-14 2021-08-19 General Electric Company Acoustic cores and methods for splicing acoustic cores

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US2821616A (en) * 1955-08-15 1958-01-28 Louis H Spott Method and apparatus for making honeycomb material
US2860740A (en) 1953-07-27 1958-11-18 Hexcel Products Inc Spliced metal foil honeycomb product and method of making same
US3549468A (en) * 1967-02-28 1970-12-22 North American Rockwell Honeycomb structure utilizing polybenzimidazole resin to join two core sections and to reinforce the edges of the cores
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EP0293320A2 (en) 1987-05-21 1988-11-30 United Technologies Corporation Two-step composite joint
US5312511A (en) * 1990-05-31 1994-05-17 Fell Barry M Apparatus for the preparation of thermoplastic honeycomb
JPH11207423A (ja) 1998-01-26 1999-08-03 Hitachi Ltd 継ぎ合わせハニカム材
US5965238A (en) 1995-11-14 1999-10-12 Kishimoto Sangyo Co., Ltd. Synthetic resin panel welding method and hollow panel structures fabricated by the method
US6039832A (en) * 1998-02-27 2000-03-21 The Boeing Company Thermoplastic titanium honeycomb panel
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Publication number Priority date Publication date Assignee Title
US2860740A (en) 1953-07-27 1958-11-18 Hexcel Products Inc Spliced metal foil honeycomb product and method of making same
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US20150267613A1 (en) * 2009-02-05 2015-09-24 Aircelle Method for manufacturing a structure with cellular cores for a turbojet nacelle
US9518509B2 (en) * 2009-02-05 2016-12-13 Aircelle Method for manufacturing a structure with cellular cores for a turbojet nacelle

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CN101903160B (zh) 2013-11-06
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RU2010134025A (ru) 2012-02-27
US20100294422A1 (en) 2010-11-25
FR2926614A1 (fr) 2009-07-24
FR2926614B1 (fr) 2010-02-12
WO2009092870A1 (fr) 2009-07-30
EP2254747B1 (fr) 2012-06-06
EP2254747A1 (fr) 2010-12-01
BRPI0821983A2 (pt) 2015-06-23
CN101903160A (zh) 2010-12-01
CA2707851A1 (fr) 2009-07-30

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